1 citations · 2 across the 4 of their papers we have counts for
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A Three-Dimensional Two-Temperature Gas-Kinetic Scheme with Generalized Kinetic Boundary Condition for Hypersonic SBLI
Xingjian Gao, Hualin Liu, Fengxiang Zhao +1
Accurate prediction of aerothermal loads in hypersonic flows is critical yet challenging due to the coupling of Shock-Wave/Boundary-Layer Interactions (SBLI) and thermal non-equili…
A two-temperature gas-kinetic scheme for hypersonic nonequilibrium flow computations
Xingjian Gao, Xing Ji, Hualin Liu +1
Accurate aerodynamic and aerothermodynamic predictions are crucial for numerous hypersonic applications. This paper proposes a gas-kinetic scheme (GKS) coupled with a two-temperatu…
On the shock wave boundary layer interaction in slightly-rarefied gas
Hualin Liu, Qi Li, Weifang Chen +1
The shock wave and boundary layer interaction (SWBLI) plays an important role in the design of hypersonic vehicles. However, discrepancies between the numerical results of high-tem…
Physical Modeling and Numerical Studies of Three-dimensional Non-equilibrium Multi-temperature Flows
Guiyu Cao, Hualin Liu, Kun Xu
For increasingly rarefied flowfields, the Navier-Stokes (NS) equations lose accuracy partially due to the single temperature approximation. To overcome this barrier, a continuum mu…